Effect of chemistry modeling on multidisciplinary hypersonic vehicle design

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn , Issue , 2010, Pages

  Starkey, Ryan P ^a  

^a University of Colorado at Boulder   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFRAME GEOMETRY; CHEMISTRY MODELING; CONVENTIONAL DESIGN; EQUILIBRIUM CHEMISTRY; INLET DESIGN; INVERSE DESIGNS; MULTI-DISCIPLINARY DESIGNS; NON EQUILIBRIUM; NONLINEAR INTERACTIONS; OPERATIONAL AIRCRAFT; PARADIGM SHIFTS; POWERED MISSILES; PROPULSION SYSTEM; SYSTEM LEVELS; THERMAL PROTECTION SYSTEM; VEHICLE DESIGN;

CHEMICAL ANALYSIS; HYPERSONIC AERODYNAMICS; HYPERSONIC VEHICLES; PROPULSION; STRUCTURAL DYNAMICS; VEHICLES;

DESIGN;

EID: 84855638462     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

1. McRuer, D.," Design and Modeling Issues for Integrated Airframe/Propulsion Control of Hypersonic Flight Vehicles, Paper WP7, 1991 American Control Conference, Boston, MA, 1991. pp. 729-735.
2. Bowcutt, K. G., "Hypersonic technology Status and Development Roadmap," AIAA HyTASP Program Committee, Technical Fellowship Advisory Board Study, December 18, 2003.
3. Chavez, F. R., and Schmidt, D. K., "Analytical Aeropropulsive/ Aeroelastic Hypersonic-Vehicle Model with Dynamic Analysis," Journal of Guidance, Control & Dynamics, Vol. 17, No. 6, November-December 1994, pp. 1308-1319.
4. Starkey, R. P., and Lewis, M. J., "Sensitivity of Hydrocarbon Combustion Modeling for Hypersonic Missile Design", AIAA Journal of Propulsion and Power, Vol. 19, No. 1, Jan-Feb 2003, pp. 89-97.
5. Starkey, R. P., Liu, D. D., Baldelli, D. H., Chang, R., Chen, P. C., "Multidisciplinary Design Optimization of a Hypersonic Air-Breathing Missile", AIAA-2007-1854.
6. O'Brien, T. F., Starkey, R. P., and Lewis, M. J., "Quasi-One- Dimensional High Speed Engine Model With Finite Rate Chemistry," AIAA Journal of Propulsion and Power, Vol. 17, No. 6, Nov-Dec 2001, pp. 1366-1374.
7. Byrne, G.D., Hindmarch, A.C., and Brown, P.N., "VODPK: Variable-Coefficient Ordinary Differential Equation Solver with the Preconditioned Krylov Method GMRES for the Solution of Linear Systems," Lawrence Livermore National Lab, . Livermore, CA, 1997.
8. Kee, R.J., Rupley, F.M., And Miller, J.A., "Chemkin-II: A Fortran Chemical Kinetics Package for the Analysis of Gas Phase Chemical Kinetics," SAND 89-8009B, Sandia National Labs., Livermore, CA, 1989.
9. Kundu, K.P., Penko, P.F. and Yang, S.L., "Reduced Reaction Mechanism for Numerical Calculations in Combustion of Hydrocarbon Fuels," AIAA Paper 98-0803, Jan. 1998.
10. Lewis, M.J., and Chang, J.S., "Joint Jet-A/Silane/Hydrgoen Reation Mechanism," Journal of Propulsion and Power, Vol. 16, No. 2, 2000. pp.365-367.
11. Rogers, R.C., "Mixing of Hydrogen Injected from Multiple Injectors Normal to a Supersonic Airstream," NASA TN D-6476, Sept. 1971.
12. Henry, J.R., Anderson, G.Y., "Design Considerations for the Airframe-Integrated Scramjet," NASA TM X-2895, Dec. 1973.
13. Starkey, R. P., "Off-design Performance Characterization of a Variable Geometry Scramjet," ISABE-2005-1111, 17th International Symposium on Airbreathing Engines, September 4-9, 2005, Munich, Germany.